FR2975179B1 - METHOD FOR AUTOMATICALLY MANAGING A LONGITUDINAL GYROMETER MOUNTED ON A FLYING DEVICE - Google Patents
METHOD FOR AUTOMATICALLY MANAGING A LONGITUDINAL GYROMETER MOUNTED ON A FLYING DEVICEInfo
- Publication number
- FR2975179B1 FR2975179B1 FR1101455A FR1101455A FR2975179B1 FR 2975179 B1 FR2975179 B1 FR 2975179B1 FR 1101455 A FR1101455 A FR 1101455A FR 1101455 A FR1101455 A FR 1101455A FR 2975179 B1 FR2975179 B1 FR 2975179B1
- Authority
- FR
- France
- Prior art keywords
- longitudinal
- flying device
- automatically managing
- gyrometer
- gyrometer mounted
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
- G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
- G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
- G01C21/183—Compensation of inertial measurements, e.g. for temperature effects
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/02—Stabilising arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/01—Arrangements thereon for guidance or control
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C25/00—Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1101455A FR2975179B1 (en) | 2011-05-13 | 2011-05-13 | METHOD FOR AUTOMATICALLY MANAGING A LONGITUDINAL GYROMETER MOUNTED ON A FLYING DEVICE |
EP12290158.0A EP2522956B1 (en) | 2011-05-13 | 2012-05-09 | Method for automatically managing a pitch rate gyro mounted on a aircraft |
ES12290158T ES2764104T3 (en) | 2011-05-13 | 2012-05-09 | Automatic management procedure for a longitudinal gyrometer mounted on a flying apparatus |
PCT/FR2012/000183 WO2012156594A1 (en) | 2011-05-13 | 2012-05-09 | Method for automatically managing a pitch rate gyroscope mounted on a flying device |
US14/115,999 US9086284B2 (en) | 2011-05-13 | 2012-05-09 | Method for automatically managing a pitch rate gyroscope mounted on a flying device |
RU2013149295/11A RU2589508C2 (en) | 2011-05-13 | 2012-05-09 | Method for automatic control pitch angular speed using gyroscopic sensor installed on aircraft |
IL229278A IL229278A (en) | 2011-05-13 | 2013-11-06 | Method for automatically managing a pitch rate gyroscope mounted on a flying device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1101455A FR2975179B1 (en) | 2011-05-13 | 2011-05-13 | METHOD FOR AUTOMATICALLY MANAGING A LONGITUDINAL GYROMETER MOUNTED ON A FLYING DEVICE |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2975179A1 FR2975179A1 (en) | 2012-11-16 |
FR2975179B1 true FR2975179B1 (en) | 2013-06-07 |
Family
ID=46062189
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1101455A Expired - Fee Related FR2975179B1 (en) | 2011-05-13 | 2011-05-13 | METHOD FOR AUTOMATICALLY MANAGING A LONGITUDINAL GYROMETER MOUNTED ON A FLYING DEVICE |
Country Status (7)
Country | Link |
---|---|
US (1) | US9086284B2 (en) |
EP (1) | EP2522956B1 (en) |
ES (1) | ES2764104T3 (en) |
FR (1) | FR2975179B1 (en) |
IL (1) | IL229278A (en) |
RU (1) | RU2589508C2 (en) |
WO (1) | WO2012156594A1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IL207536A (en) | 2010-08-11 | 2016-11-30 | Israel Aerospace Ind Ltd | System and method for measurement of angular orientation of aerospace platforms |
CN104596545B (en) * | 2015-01-27 | 2017-07-28 | 北京航天时代光电科技有限公司 | A kind of fiber-optic inertial measurement apparatus gyroscope scale factor Temperature Modeling method |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3925643A (en) * | 1974-05-13 | 1975-12-09 | United Technologies Corp | Drift correcting gyro system using filters |
US3925642A (en) * | 1974-05-13 | 1975-12-09 | United Technologies Corp | Strapdown gyro drift calculator |
US4017187A (en) * | 1975-06-23 | 1977-04-12 | Sperry Rand Corporation | Double rotation inertial measurement apparatus |
US4343035A (en) * | 1980-04-14 | 1982-08-03 | Tanner Walter E | Heading reference system |
GB8512340D0 (en) * | 1985-05-15 | 1986-10-29 | Gec Avionics | Measuring dynamic system |
US5442442A (en) * | 1987-10-28 | 1995-08-15 | Litton Systems, Inc. | Ring laser gyroscope scale factor error control apparatus and method control apparatus and method |
EP0392104A1 (en) * | 1989-04-13 | 1990-10-17 | Litton Systems, Inc. | Inertial navigation system |
US5194872A (en) * | 1990-11-14 | 1993-03-16 | Charles Stark Draper Laboratory, Inc. | Inertial navigation system with automatic redundancy and dynamic compensation of gyroscope drift error |
JPH07324941A (en) * | 1994-06-02 | 1995-12-12 | Matsushita Electric Ind Co Ltd | Correction apparatus of offset drift |
US5941935A (en) * | 1996-09-23 | 1999-08-24 | Fernandez; Manuel | Azimuth-axis drift rate determination in an inertial navigator |
US6032099A (en) * | 1996-11-02 | 2000-02-29 | Fernandez; Manuel | Automatic correction of key error sources in an inertial navigator |
FR2826447B1 (en) * | 2001-06-26 | 2003-09-19 | Sagem | HYBRID INERTIAL NAVIGATION METHOD AND DEVICE |
FR2910615B1 (en) * | 2006-12-20 | 2009-02-06 | Sagem Defense Securite | METHOD OF CALIBRATING THE SCALE FACTOR OF AN AXISYMETRIC VIBRATION GYROMETER |
US8519313B2 (en) * | 2008-12-01 | 2013-08-27 | Raytheon Company | Projectile navigation enhancement method |
-
2011
- 2011-05-13 FR FR1101455A patent/FR2975179B1/en not_active Expired - Fee Related
-
2012
- 2012-05-09 EP EP12290158.0A patent/EP2522956B1/en active Active
- 2012-05-09 US US14/115,999 patent/US9086284B2/en not_active Expired - Fee Related
- 2012-05-09 WO PCT/FR2012/000183 patent/WO2012156594A1/en active Application Filing
- 2012-05-09 ES ES12290158T patent/ES2764104T3/en active Active
- 2012-05-09 RU RU2013149295/11A patent/RU2589508C2/en active
-
2013
- 2013-11-06 IL IL229278A patent/IL229278A/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
RU2589508C2 (en) | 2016-07-10 |
RU2013149295A (en) | 2015-06-20 |
US9086284B2 (en) | 2015-07-21 |
US20140158813A1 (en) | 2014-06-12 |
ES2764104T3 (en) | 2020-06-02 |
EP2522956B1 (en) | 2019-11-20 |
FR2975179A1 (en) | 2012-11-16 |
IL229278A (en) | 2017-05-29 |
IL229278A0 (en) | 2014-01-30 |
WO2012156594A1 (en) | 2012-11-22 |
EP2522956A1 (en) | 2012-11-14 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 5 |
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PLFP | Fee payment |
Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |
|
ST | Notification of lapse |
Effective date: 20220105 |